JASC 5414
Service difficulty reports · 4,360
Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5414' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5414' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SIMA20150401006Skin · chafedPYLON SKIN IS CHAFED FROM THE STEEL BRAIDED LANYARD INSIDE ACCESS PANEL 414DB. COMPLIED WITH PYLON SKIN REPAIR INSIDE ACCESS PANEL 414DB IAW ERS-54MR-309.SDR IPXA2015040287656Skin · damagedINSPECTION TYPE:C, NR 1 PYLON INBD SKIN DAMAGE. REPAIRED NR 1 PYLON INBD SKIN, PN 311N5046-34 IAW EA 757-5451-27-A2172 AND EO B757-5430-57073-A.SDR REXA2015032600369Skin · crackedTASK CARD CRJ 900, PANEL 443 BT IS CRACK & CHAFED. R & R PANEL 443 BT SKIN IAW SRM 51-42-06-001-001-A01.SDR HALA2015032500042Skin · puncturedETOPS SIGNIFICANT SYS - NR 1 ENGINE HAS A SMALL PUNCTURE IN THE INNER SKIN OF THE NOSE
COWL AT THE 11:00 POSITION. JUST AFT OF THE EEC COOLING INLET. DEFERRED IAW ERA 534614-14 , REPAIRED APPROVED AND TIME LIMITED IAW PS 900-5-1, NR 4. C/W MAINT PROCEDURESDR SWIA201540995Skin · puncturedLEFT UPPER PYLON HAS A PUNCTURE APPROX. 15" FROM T/E. COMPLIED WITH TEMPORARY REPAIR IAW SRM. PERMANENT REPAIR DUE AT NEXT C-CHECK. C-CHECK RO 4/7/15. REPAIRED LT PYLON UPPER SKIN IAW STS EA PERMANENT REPAIR STEPS 1A-1C, D: COMPLIED WITH ST 51-900-1000.SDR IPXA2015040287654Skin · crackedINSPECTION TYPE:3C, 2 PYLON LOWER FWD SKIN PANEL RT SIDE CRACKED WITH SHEARED FASTENER. REPAIRED NR 2 PYLON SKIN PANEL IAW SRM 54-00-00, FIG 204.SDR CALA2015032093448Skin Panel · crackedSUSPECT CRACK IN PYLON SKIN AT PANEL CUT OUT UPPER LT CORNER THRU RIVET. NEED QC DEPARTMENT TO ACCOMPLISH HFEC TO CONFIRM. PERFORMED HFEC INSPECTION TO SUSPECTED CRACK LOCATION IAW NDT PART 6 51-00-19. VERIFIED THE LENGTH OF CRACK MARKED WHERE CRACK STOPS PSDR FDEA201503180973Skin · damagedNUMBER 2 ENG RT FAN COWL, FWD LOWER JAMB AREA GOUGED. SKIN REPAIR IAW SRM 54-20-15 FIG 201 REPAIR 1.SDR ASAA2015030611098Skin · crackedPOSSIBLE CRACK NR 2 PYLON AT PANEL 5823R OPENING LOWER FWD CORNER. ACFT GROUNDED. REPAIRED CRACKED NR 2 PYLON AT PANEL 5823R OPENING FWD CORNER IAW SRM 54-50-01-2R-2 REPAIR 2.SDR K11A2015031325008Skin · crackedNR 1 PYLON FASTENER HOLE "P" HAS CRACK INDICATION, REF SB 727-54A0010.SDR REXA2015022400266Skin · damagedNUMBER 2 ENG HINGE LINE FAIRING 443BT CHAFED & CRACKED AROUND FASTENER HOLE. LOCATED & DRILLED NEW FAIRING SKIN IAW SRM 51-40-11-001-001-A01. REMOVED & REINSTALLED STIFFENERS IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01. APPLIED TOP COAT TO NEW FAIRISDR REXA2015022400265Fairing · chafedNUMBER 1 ENG PYLON HINGE LINE FAIRING 433BB HAS CHAFE DAMAGE. LOCATED & DRILLED NEW FAIRING SKIN IAW SRM 51-40-11-001-001-A01. REMOVED & INSTALLED STIFFENERS IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01. APPLIED TOP COAT TO NEW FAIRING IAW SRM 51-25-SDR CALA2015022693178Access Panel · crackedNUMBER 1 PYLON RT ACC PANEL 452ER CUT OUT LOWER AFT EDGE FOUND CRACK. REPAIRED IAW ECRA 5430-02019.SDR DALA2015022301794Skin · crackedNR 1 ENGINE PYLON, TRAPEZOIDAL PANEL 436BR, INBD SIDE OF PYLON, PYLON CUT OUT SKIN CRACKED, FWD EDGE, ERA 533148-14.SDR DALA2015022301793Skin · crackedNR 1 ENGINE PYLON, PANEL 436BL, OTBD SIDE OF PYLON, PYLON CUT OUT SKIN CRACKED, FWD EDGE. REPAIRED IAW ERA 533-149-14.SDR UIEA2015020600082Skin · crackedNUMBER 1 PYLON SKIRT FAIRING INBD SKIN CRACK FOUND AT ADP EXHAUST GRILL UPPER AFT SCREW HOLE AREA. REPAIRED IAW R1-54-00-10797 REV A.SDR UIEA2015020900106Skin · crackedNUMBER 2 ENG RT CORE COWL, EXTERNAL SKIN CRACK FOUND JUST BELOW PRE COOLER EXHAUST GRILL. REPAIRED IAW SRM 54-45-01-2R-4 REPAIR 4.SDR DALA2015020200977Skin · crackedNR 1 PYLON, OTBD SIDE STRUT ASSY. SKIN AT UPPER AFT CORNER OF 442AL ACCESS DOOR CUTOUT CRACKED. C/W PRI 532568-14.SDR DALA2015020400969Skin · crackedNR 2 PYLON AFT LOWER STRUT ACCESS DOOR 446BL CUTOUT AREA FOUND CRACKED. REMOVED AND INSTALLED FILLER IAW SRM 54-53-01.SDR COEA2015012701913Cover · missingAIRCRAFT LANDED NORMALLY WITHOUT INCIDENT. DURING POST FLIGHT INSPECTION, THE FIRST OFFICER NOTED THAT THE NR 2 ENG OTBD COWLING COVER WAS MISSING. AT NO POINT DURING THE FLIGHT WERE ANY IRREGULARITIES APPARENT TO THE CREW. INSTALLED MISSING NR 2 ENG OTBD CSDR CALA2015011392946Skin · crackedNUMBER 1 PYLON RT ACCESS DOOR 452ER LOWER AFTER CUT OUT FOUND CRACK APPROX 1 INCH LONG. NR 1 PYLON RT ACCESS DOOR 452ER LOWER AFTER CUT OUT REPAIRED IAW ECRA 5430-02013.SDR CA150107001Cowling · missing(CAN) MISSING PIECE OF COWLING. CLEARANCE WAS ISSUED. NO EMERGENCY DECLARED AND FLIGHT LANDED. ONCE INSPECTED BY MAINTENANCE IT WAS CONFIRMED THAT LT UPPER AFT COWLING PN 114-980078-21 WAS MISSING. IT WAS DETERMINED THAT THE COWLING WAS ONLY PUT IN PLACE BY SDR KO0R201412290031Skin · crackedNR 3 PYLON INBD EXTERNAL SKIN IS CRACKED AT THE UPPER FORWARD CORNER OF ACCESS HOLE FOR PANEL 473FL AT NACELLE, STA 207, NACELLE, WL 150.SDR SWIA201440478Skin · dentedLT NACELLE HAS TWO SMALL DENTS IN CENTER AREA OF FAN COWL. REPAIRED IAW EA.SDR SWIA201440477Skin · dentedLT NACELLE TWO DENTS ON NOSE COWL. REPAIRED IAW EA.SDR SWIA201440476Skin · dentedLT NACELLE HAS ONE TWELVE INCH LONG DENT AT FWD END OF FAN COWL. REPAIRED IAW EA.SDR SWIA201440475Skin · dentedLT NACELLE HAS ONE SMALL DENT AT 4:30 O-CLOCK POSITION ON CENTER AREA OF AFT CORE COWL. COMPLIED WITH EA.SDR REXA2014121801221Skin · damagedNR 2 ENGINE AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. MECH REMOVED DAMAGE AT PYLON INTERFACE AREA, FABRICATED RUB STRIPS. PERFORMED NDT AND INSTALLED RUB STRIPS IAW SRM 54-13-00-201-006-A01 AND NDTM PART 1 51-20-006-25-A01, SRM 51-42-06-001-00SDR REXA2014121701216Skin · damagedNR 1 ENGINE AFT CORE COWL STAND OF BLOCK AT 3 O'CLOCK POSITION HAS DAMAGE ALIGNMENT TAB. MECH R & R STANDOFF BLOCK AND INSULATION PAD AT NR 1 ENGINE AFT CORE COWL AT 3 O'CLOCK POSITION IAW SRM 54-13-00-201-002-A01.SDR CALA2014122392854Skin · crackedNUMBER 1 STRUT TORQUE BOX SKIN AT ACCESS DOOR 452ER HAD 1 INCH CRACK AT LOWER AFT CORNER. REPAIR OF SKIN CRACK WAS ACCOMPLISHED IAW ECRA 5450-02283.SDR SWIA201440473Skin · dentedLEFT ENGINE LOWER COWL HAS SEVERAL DENTS. REPAIRED IAW EA.SDR CALA2014122392834Skin · crackedNUMBER 2 PYLON STRUT INBD SIDE SKIN AT AFT TRAPEZOIDAL ACCESS DOOR 446BL IS CRACKED ON FWD UPPER CORNER. STOP DRILLED CRACK, INSTALLED SCAB DOUBLER REPAIR IAW SRM54-53-01 REPAIR 7.SDR FDEA201412114105Panel · delaminatedPANEL 364 DR RT PICKLE BARREL HAS MINOR DAMAGE. REPAIRED PANEL 364 DR RT PANEL IAW SRM 51-71-00 VOL II.SDR DALA2014120906455Skin · crackedFOUND LT PYLON INBD STRUT SIDE SKIN PANEL CRACKED AT NAC STA 166 ACCESS DOOR CUTOUT. DRILLED STOP HOLE AT THE END OF CRACKED AREA IAW SRM 51-10-00. REPAIR PARTS MADE AS SRM 54-53-01, FIG 201.SDR REXA2014120701172Fairing · crackedTASK CARD C1 NR 2 ENG UPPER HINGE LINE FAIRING SHOWS CRACK AROUND FASTENER HOLE. R & R NR 2 ENG UPPER HINGE FAIRING SKIN IAW SRM 51-42-06-001-001-A01.SDR SWIA201440395Skin · dentedLT CORE COWL DENTED FORWARD OF CARGO DOOR. REMOVED, REINSTALLED, EVALUATED AND REPAIRED LT LOWER FAN COWL DOOR REF REO.SDR SWIA201440307Skin · failedLEFT ENGINE, LOWER COWL NYLON INSERT THAT THE TRANSLATING COWL SLIDER MOVES ON, THE SCREWS THAT HOLD THE INSERT IN PLACE HAVE BACKED OUT AND STRIKE THE SLIDER. MARKED. C-CHECK, REPAIRED LT LOWER NYLON INSERT SCREWS IAW REO.SDR SWIA201440306Skin · gougedLT ENGINE INBD LOWER TRANSLATING COWL SLIDER GOUGED AT FORWARD END. MARKED, C-CHECK, RO 12/6/14. REMOVED DAMAGE FROM LT INBD LOWER TRANSLATING COWL SLIDER AT FORWARD END. ORIGINAL MATERIAL THICKNESS .152", REMAINING THICKNESS .114". MATERIAL LOSS OF .038" SDR SWIA201440304Skin · dentedLEFT ENGINE COWLING, FAN COWL HAS SEVERAL DENTS 6:00 POSITION TO 8:00 POSITION. C-CHECK, RO 12/6/14. REPAIRED DENTS ON LT ENGINE FAN COWL AT 06:00 TO 8:00 POSITIONS IAW REO ALL STEPS, WITHIN LIMITS.SDR SWIA201440226Skin · damagedLEFT ENGINE LOWER COWL AT 5 O`CLOCK, 2" AFT AND 1" INBD OF EXISTING SCAB PATCH. SHALLOW DENT, SCRATCH. PLEASE EVALUATE AND OR REPAIR AS NECESSARY. C-CHECK, RO 11/30/14, REWORKED LT ENGINE LOWER FAN COWL DOOR REF REO. NO DEFECTS NOTED REF NDT ITEM 5, NO "OISDR SWIA201439910Skin · damagedRIGHT ENGINE LOWER COWL DAMAGED. R & R RT ENGINE INLET COWL IAW AMM.SDR FDEA201411083592Panel · crackedRIGHT PYLON PANEL 457BT CRACKED AS MARKED. PANEL RACK WELDED ON T14 1102142 IAW EA 8-5480-T0312625 REV NO PS P 1. NACELLES & PYLON FILLETS FAIRINGS RT PYLON PANEL 457BT CRACKED. MINOR REPAIR.SDR SWIA201440088Skin · dentedDENT ON LT ENGINE LOWER FAN COWL,. FOUND TO BE WITHIN LIMITS, IAW REO.SDR SWIA201439895Skin · chafedLT ENGINE UPPER FAN COWL HAS A CHAFING. C-CHECK, REPAIRED CHAFE DAMAGE TO LT ENGINE UPPER FAN COWL IAW STS EA.SDR CALA2014102792618Skin · damagedNUMBER 1 ENG LT & RT TR'S LOWER INNER AFT BIFURCATION FAIRING S SKIN FOUND PITTED DURING GSO C-16 VISIT. AFTER DAMAGE REMOVAL & BLENDING REMAINING MATERIAL IS .081 INCHES WITH .019 INCHES REMOVED, OUT OF LIMITS OF SRM 54-33-01. WORK STEPS OF ECRA 7830-02831 SDR SWIA201439666Skin · dentedRT ENGINE COWL IS DENTED OUT OF LIMITS. REPLACED IAW AMM.SDR FDEA201410193310Skin · wornNUMBER 2 ENG LOWER RT AFT PICKLE BARREL SECTION, PANEL WORN THROUGH AT APPROX 5:30 POSITION, FWD OF CSD, MARKED. REMOVED DAMAGED SKIN SECTION BELOW PREVIOUSLY, ACCOMPLISHED SPLICE REPAIR IAW SRM 51-31-01 VOL 2. FABRICATED REPLACEMENT SKIN SECTION IAW SRM 54SDR SWIA201439741Skin · dentedLT ENGINE LOWER FAN COWL DOOR HAS SEVERAL DENTS AT 6 O'CLOCK POSITION. REPAIRED LT ENGINE LOWER FAN COWL DOOR DENTS IAW REO.SDR SWIA201439859Skin · chafedLEFT ENGINE CORE COWL, 435AB HAS 3.5 INCH CHAFE AFT OF FWD LATCH. C-CHECK, REPAIRED LT ENGINE CORE COWL 435AB IAW STS EA.SDR SWIA201439736Skin · dentedSEVERAL DENTS ON LT ENGINE LOWER NOSE COWL AND FAN COWL DOORS AT 6 O'CLOCK POSITION. COMPLIED WITH THE REPAIR OF SEVERAL DENTS ON THE LT ENGINE LOWER NOSE COWL AND FAN COWL DOORS AT THE 6 O'CLOCK POSITION IAW EA.
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